ERA13LA175 · Mooney M20F
Mooney M20F · Accident: system/component malfunction/failure (non-power) while maneuvering
From Leesburg International Airport (LEE) to Leesburg International Airport (LEE)
Event
- NTSB case
- ERA13LA175
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- Unknown
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Mooney M20F
- Aircraft type
- Mooney M20
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N9387V
- Operator
- Paul S Soule · private individual
- Onboard fatalities
- Unknown
- Route
- From Leesburg International Airport (LEE), Leesburg, FLTo Leesburg International Airport (LEE), Leesburg, FL
- Aircraft age
- Not recorded
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- Maneuvering
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- System/component malfunction/failure (non-power)
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Aircraft › Aircraft systems
- Personnel issues › Task performance
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The pilot reported that when he attempted to extend the landing gear, he heard a "snap," and the landing gear did not extend. He then cycled the landing gear and attempted the emergency (manual) landing gear extension procedure with no success. The pilot subsequently performed a gear-up landing to a grassy area at an airport. Examination of the airplane revealed that the emergency gear extension cable terminated with a spline drive at the landing gear actuator. The emergency cable was separated from the spline drive, which was seized. The emergency gear extension cable was also misrigged, which allowed it to contact the landing gear actuator arm and engage the cable during normal gear operations. Subsequently, with a seized spline engaged to the electric landing gear motor via the actuator, during normal gear operations, the electric landing gear motor would not be able to overcome the seized spline to actuate the landing gear.
The airplane had been operated about 60 hours since its most recent annual inspection, which was completed about 10 months before the accident. Review of the airplane's most recent airframe logbook (dating back 7 years) revealed that the landing gear actuator was removed and replaced about 4 years before the accident. During reinstallation of the actuator, an emergency (manual) gear extension was successfully completed. There were no other entries pertaining to emergency (manual) gear extension in the airframe logbook; however, the entry for the most recent 100 hour inspection noted three landing gear retraction cycles. The mechanic that recorded that entry stated it was a standard entry and typically more than three cycles are completed with the first one being the emergency (manual) extension. While it was likely that a mechanic checked the rigging of the emergency gear extension cable following the actuator replacement, the investigation was unable to determine if the rigging of the emergency gear extension cable was affected by any subsequent maintenance. Additionally, the cable routing and rigging wouldn't typically be inspected if the landing gear manual extension was successfully accomplished during the 100-hour or annual inspections.
Probable cause
The incorrect rigging of the landing gear emergency extension system by unknown maintenance personnel, which resulted in a failure of the emergency extension cable, and jamming of the normal extension gear motor.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA13LA175
- Event ID
- 20130320X04251
- Case number
- ERA13LA175
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: d05778f2b65881747e59d6a422457d1dc93528606f028674f2dcef6e7adf7094; retrieved 2026-09-15T21:08:25.368Z.